Influence of the inclined leading edge diffuser vanes on the aerodynamic performance of a transonic centrifugal compressor
Crossref DOI link: https://doi.org/10.1007/s12206-017-1050-z
Published Online: 2017-11-21
Published Print: 2017-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Zamiri, Ali
Lee, Byung Ju
Chung, Jin Taek
License valid from 2017-11-01
